STRUCTURAL DESIGN, ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE

This project and dissertation is a significant outcome of supreme guidance and concentrated team effort. We respectfully acknowledge the cordial help of individuals who played distinct role for the successful accomplishment of the project. We offer our deepest gratitude to our supervisor Wg Cdr Dr G...

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Autors principals:	Rahman, Irfanur, Asaduzzaman, K. M., Arman, Arif
Format:	Thesis
Idioma:	anglès
Publicat:	Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST) 2016
Matèries:	STRUCTURAL DESIGN, ANALYSIS, FLIGHT, UNMANNED AERIAL VEHICLE, AEROFOIL, SHAPED FUSELAGE
Accés en línia:	http://hdl.handle.net/123456789/245
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